MIL-STD-2066 Base Document:1981
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066)
20-03-1981
17-03-1999
Criteria for calculating catapulting and arresting loads for design of US airplanes (Naval).
| DocumentType |
Standard
|
| Pages |
186
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
The information contained herein presents loading characteristics, associated parameters, and methods to be used in calculating the catapulting and arresting loads of MIL-A-8863 and MIL-A-8866 for the design of U.S. Navy airplanes operating from shipboard and shorebased launching and recovery gears. A listing of such gears for which data is contained herein is given in Table 1.
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
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